US11260566B2ActiveUtilityA1

Methods to increase structural performance, strength and durability of fabric-reinforced composite materials by pre-stressing

63
Assignee: UNIV MICHIGAN REGENTSPriority: Sep 15, 2014Filed: Jan 17, 2020Granted: Mar 1, 2022
Est. expirySep 15, 2034(~8.2 yrs left)· nominal 20-yr term from priority
D06M 15/507D06M 15/564D04B 37/02D06M 15/55D10B 2505/02D06M 2101/36D06M 15/59D04B 1/102B29K 2995/0077B29C 70/56D06M 2101/20D06M 2101/40B29B 11/16B29C 70/22D04B 1/22B29K 2709/08B29K 2995/0087D06M 15/70D06B 1/10B29C 45/1418D06M 15/41B29C 45/7207B29C 70/48D04B 15/66B29K 2063/00B29K 2105/0836
63
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Cited by
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References
18
Claims

Abstract

Methods to increase structural performance, strength, and durability of textile-reinforced composite materials are provided. The textile reinforcement may be knitted, for example, in a flat bed weft knitting machine. The method may include pre-stressing a textile reinforcement preform by applying tension. A polymeric precursor may be introduced to the pre-stressed textile reinforcement preform. The polymeric precursor may then be cured or consolidated, followed by releasing of the applied tension to form the composite article comprising polymer and the pre-stressed textile reinforcement. In other aspects, a composite article is provided that has a pre-stressed textile reinforcement structure and a cured polymer. The textile reinforcement may be a knitted, lightweight, seamless, unitary structure. The knitted reinforcement structure may have distinct first and second knitted regions with different levels of pre-stress, thus providing enhanced control over strength, rigidity, and flexibility of the composite article.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
       1. A method of making a load bearing composite article comprising:
 placing a textile reinforcement preform into a three-dimensional formwork, wherein the composite article has a shape defined by the three-dimensional formwork; 
 pre-stressing the textile reinforcement preform by applying uniaxial tension thereto; 
 introducing a liquid polymeric precursor into the pre-stressed textile reinforcement preform to partially or fully fill openings in the textile reinforcement preform after the textile reinforcement preform is placed into the three-dimensional formwork; 
 curing the polymeric precursor; and 
 releasing the applied tension to form the load bearing composite article comprising a cured polymer embedding the pre-stressed textile reinforcement. 
 
     
     
       2. The method of  claim 1 , further comprising forming the textile reinforcement preform prior to the pre-stressing. 
     
     
       3. The method of  claim 2 , wherein the forming comprises knitting the textile reinforcement preform into a unitary seamless structure. 
     
     
       4. The method of  claim 3 , wherein the knitting is conducted on a computer numerical control (CNC) flat bed weft knitting machine. 
     
     
       5. The method of  claim 3 , wherein the knitting forms a first knitted region and a distinct second knitted region in the textile reinforcement preform, wherein the first knitted region and the second knitted region vary from one another by at least one property selected from the group consisting of: stitch pattern, stitch density, stitch length, stitch spacing, yarn composition, yarn thickness, yarn denier, yarn weight, yarn ply, yarn degree of twist, rigidity, flexibility, and combinations thereof. 
     
     
       6. The method of  claim 1 , wherein the introducing of the polymeric precursor is only to select regions of the pre-stressed textile reinforcement preform. 
     
     
       7. The method of  claim 1 , wherein the introducing of the polymeric precursor is to the entire pre-stressed textile reinforcement preform. 
     
     
       8. The method of  claim 1 , wherein the knitted reinforcement structure comprises a first knitted region and a distinct second knitted region, and the pre-stressing creates a first pre-stress level in the first knitted region and a second pre-stress level in the distinct second knitted region that is greater than the first pre-stress level. 
     
     
       9. The method of  claim 8 , wherein the first knitted region has a first rigidity level and the second knitted region has a second rigidity level, wherein the first rigidity level is at least 25% greater than the second rigidity level. 
     
     
       10. The method of  claim 1 , wherein the liquid polymeric precursor forms a cured thermoset polymer selected from the group consisting of: epoxies, polyesters, polyimides, phenols, bismaleimides, polyurethanes, derivatives, copolymers, and combinations thereof. 
     
     
       11. The method of  claim 1 , wherein the pre-stressed seamless knitted reinforcement structure comprises a yarn selected from the group consisting of: carbon fiber, glass fiber, polymeric fibers, metal fibers, and combinations thereof. 
     
     
       12. The method of  claim 1 , wherein the pre-stressed seamless knitted reinforcement structure comprises a yarn selected from the group consisting of: carbon fiber, glass fiber, aramid fibers, polyelastane fibers, polyolefin fibers, thermoplastic monofilaments, and combinations thereof. 
     
     
       13. A method of making a load bearing composite article comprising:
 placing a textile reinforcement preform into a three-dimensional formwork, wherein the composite article has a shape defined by the three-dimensional formwork; 
 pre-stressing the textile reinforcement preform by applying uniaxial tension thereto; 
 introducing a liquid polymeric precursor into the pre-stressed textile reinforcement preform to partially or fully fill openings in the textile reinforcement preform after the textile reinforcement preform is placed into the three-dimensional formwork; 
 curing the polymeric precursor; and 
 releasing the applied tension to form the load bearing composite article comprising a cured polymer embedding the pre-stressed textile reinforcement, wherein the load bearing composite article is a structural component for at least one of an automotive structure, an aerospace structure, a rail structure, a ship structure, a transportation structure, an infrastructure structure, or an architectural structure. 
 
     
     
       14. The method of  claim 13 , wherein the forming comprises knitting the textile reinforcement preform into a unitary seamless structure. 
     
     
       15. The method of  claim 14 , wherein the knitting is conducted on a computer numerical control (CNC) flat bed weft knitting machine. 
     
     
       16. The method of  claim 14 , wherein the knitting forms a first knitted region and a distinct second knitted region in the textile reinforcement preform, wherein the first knitted region and the second knitted region vary from one another by at least one property selected from the group consisting of: stitch pattern, stitch density, stitch length, stitch spacing, yarn composition, yarn thickness, yarn denier, yarn weight, yarn ply, yarn degree of twist, rigidity, flexibility, and combinations thereof. 
     
     
       17. The method of  claim 13 , wherein the introducing of the polymeric precursor is only to select regions of the pre-stressed textile reinforcement preform. 
     
     
       18. The method of  claim 13 , wherein the introducing of the polymeric precursor is to the entire pre-stressed textile reinforcement preform.

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